HITCAN for Actively Cooled Hot-Composite Thermostructural AnalysisSource: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002::page 315DOI: 10.1115/1.2906589Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A computer code, HITCAN (High Temperature Composite Analyzer) has been developed to analyze/design hot metal matrix composite structures. HITCAN is a general purpose code for predicting the global structural and local stress-strain response of multilayered (arbitrarily oriented) metal matrix structures both at the constituent (fiber, matrix, and interphase) and the structure level and including the fabrication process effects. The thermomechanical properties of the constituents are considered to be nonlinearly dependent on several parameters, including temperature, stress, and stress rate. The computational procedure employs an incremental iterative nonlinear approach utilizing a multifactor-interaction material behavior model, i.e., the material properties are expressed in terms of a product of several factors that affect the properties. HITCAN structural analysis capabilities (static, load stepping—a multistep static analysis with material properties updated at each step, modal, and buckling) for cooled hot structures are demonstrated through a specific example problem.
keyword(s): Composite materials , Stress , Materials properties , Design , Computers , Buckling , High temperature , Fibers , Manufacturing , Metal matrix composites , Temperature , Metals AND Structural analysis ,
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| contributor author | C. C. Chamis | |
| contributor author | S. N. Singhal | |
| contributor author | J. J. Lackney | |
| contributor author | P. L. N. Murthy | |
| date accessioned | 2017-05-08T23:38:27Z | |
| date available | 2017-05-08T23:38:27Z | |
| date copyright | April, 1992 | |
| date issued | 1992 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26699#315_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/110242 | |
| description abstract | A computer code, HITCAN (High Temperature Composite Analyzer) has been developed to analyze/design hot metal matrix composite structures. HITCAN is a general purpose code for predicting the global structural and local stress-strain response of multilayered (arbitrarily oriented) metal matrix structures both at the constituent (fiber, matrix, and interphase) and the structure level and including the fabrication process effects. The thermomechanical properties of the constituents are considered to be nonlinearly dependent on several parameters, including temperature, stress, and stress rate. The computational procedure employs an incremental iterative nonlinear approach utilizing a multifactor-interaction material behavior model, i.e., the material properties are expressed in terms of a product of several factors that affect the properties. HITCAN structural analysis capabilities (static, load stepping—a multistep static analysis with material properties updated at each step, modal, and buckling) for cooled hot structures are demonstrated through a specific example problem. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | HITCAN for Actively Cooled Hot-Composite Thermostructural Analysis | |
| type | Journal Paper | |
| journal volume | 114 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.2906589 | |
| journal fristpage | 315 | |
| journal lastpage | 320 | |
| identifier eissn | 0742-4795 | |
| keywords | Composite materials | |
| keywords | Stress | |
| keywords | Materials properties | |
| keywords | Design | |
| keywords | Computers | |
| keywords | Buckling | |
| keywords | High temperature | |
| keywords | Fibers | |
| keywords | Manufacturing | |
| keywords | Metal matrix composites | |
| keywords | Temperature | |
| keywords | Metals AND Structural analysis | |
| tree | Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002 | |
| contenttype | Fulltext |